Experimental Steady-State Yawing Derivatives of a 60 Degree Delta-Wing Model as Affected by Changes in Vertical Position of the Wing and in Ratio of Fuselage Diameter to Wing Span
| Author: | Jaquet, Byron M. |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3843 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56175/ |